Calibration system for calibrating orientation parameters of digital optoelectronic sensors in a mobile carrier used for remote reconnaisance
    21.
    发明授权
    Calibration system for calibrating orientation parameters of digital optoelectronic sensors in a mobile carrier used for remote reconnaisance 失效
    用于校准用于远程侦察的移动运营商中的数字光电传感器的定向参数的校准系统

    公开(公告)号:US06864969B1

    公开(公告)日:2005-03-08

    申请号:US09588894

    申请日:2000-06-07

    申请人: Anko Börner

    发明人: Anko Börner

    IPC分类号: G01C11/02 G01C3/08 G01B11/26

    CPC分类号: G01C11/02

    摘要: A calibration system for ccalibrating orientation parameters of a digital optoelectronic sensor system includes an attitude and position determining system arranged in a mobile carrier, such as an airplane or a satellite, for determining the orientation parameters in flight. An optoelectronic component emits light in a defined direction with respect to the mobile carrier. A planar optical detector is arranged relative to the optoelectronic device for detecting the reflection of radiation emitted from the optoelectronic device and reflected off of a reference module arranged on the ground. The orientation parameters of the reference module are known, wherein the offsets of the orientation parameters of the attitude and position determining system may be determined by evaluating the radiation emitted by the light-emitting component, reflected from the reference module and received by the planar detector.

    摘要翻译: 用于校准数字光电传感器系统的取向参数的校准系统包括布置在诸如飞机或卫星的移动载体中的姿态和位置确定系统,用于确定飞行中的取向参数。 光电子部件相对于移动式载体在规定的方向上发光。 平面光学检测器相对于光电子器件布置,用于检测从光电子器件发射的辐射的反射并被布置在地面上的参考模块反射。 参考模块的取向参数是已知的,其中姿态和位置确定系统的取向参数的偏移可以通过评估由参考模块反射并由平面检测器接收的由发光部件发射的辐射来确定 。

    Actuator system
    22.
    发明授权

    公开(公告)号:US11625021B2

    公开(公告)日:2023-04-11

    申请号:US16832234

    申请日:2020-03-27

    发明人: Michael Panzirsch

    IPC分类号: G05B19/416

    摘要: An actuator system may include a first actuator for being operated by a user, a second actuator for performing a movement of the user, and a transmission channel between the first actuator and the second actuator for transmitting the velocity and the force of the first actuator to the second actuator and vice versa. The actuator system may also include a controller, wherein the controller is configured such that, with the aid of the controller, the energy of the first actuator is adapted to be measured as a desired energy, wherein the transmission channel is configured for transmitting the desired energy to the second actuator and the controller is configured for controlling the damping of the second actuator as a function of the desired energy.

    3-D input device
    23.
    发明授权

    公开(公告)号:US11507202B2

    公开(公告)日:2022-11-22

    申请号:US17044875

    申请日:2019-04-05

    IPC分类号: G06F3/0338

    摘要: A 3D input device, in particular a mobile 3D input device, has a housing and an input element arranged within the housing. The input element has at least a first side and a second side opposite the first side. The 3D input device has a sensor device. The input element is movable relative to the housing in six components. The sensor device detects the movements and/or the positions of the input element relative to the housing. The first side of the input element or the second side of the input element or the first side and the second side of the input element are together configured in such a way that a user can complete a movement of the input element along the six components via an action on the input element. A mobile device and a 3D remote-control each have at least one such 3D input device.

    Method of and Transonically Operating Aircraft having Devices For Suppressing Aeroelastic Instabilities

    公开(公告)号:US20220324553A1

    公开(公告)日:2022-10-13

    申请号:US17742926

    申请日:2022-05-12

    IPC分类号: B64C21/00 B64C23/04

    摘要: In order to suppress aeroelastic instabilities on a transonically operating aircraft comprising a pair of wing halves at which a transonic flow forms spatially limited supersonic flow regions that each, in a main flow direction of the flow, end in a compression shock, a boundary layer of the flow is temporarily thickened-up in at least one supersonic flow region at at least one of the two wing halves, when approaching a flight envelope of the aircraft with increasing flight Mach number of the aircraft. The boundary layer of the flow is thickened-up to such an extent that the compression shock at the end of the respective supersonic flow region at the present flight Mach number of the aircraft induces a separation of the boundary layer of the flow from the wing half.

    METHOD AND APPARATUS FOR IMPREGNATING A FIBRE BUNDLE AND METHOD AND FACILITY FOR PRODUCING A THREE-DIMENSIONAL STRUCTURE

    公开(公告)号:US20220212369A1

    公开(公告)日:2022-07-07

    申请号:US17438111

    申请日:2020-02-13

    发明人: Maik TITZE

    摘要: The invention relates to a method for impregnating at least one fibre bundle (11) with a high-viscosity plastics material (13), said method comprising the following steps: •—providing at least one fibre bundle (11) for impregnation, formed of a multiplicity of continuous fibres, and providing a plastics material (13), melted at a mandated operating temperature and of high viscosity, and •—impregnating the fibre bundle (11) with the plastics material (13), by guiding the fibre bundle for impregnation continuously through an impregnation cavity (12), filled with the melted plastics material (13), •—where during impregnation of the fibre bundle, the melted plastics material within the impregnation cavity is contacted with a surface (15) of at least one oscillation generator (14) in such a way that sonic energy is introduced by said oscillation generator into the melted high-viscosity plastics material in the impregnation cavity.

    METHOD FOR APPLYING A MATERIAL TO A FIBER COMPOSITE COMPONENT

    公开(公告)号:US20210316496A1

    公开(公告)日:2021-10-14

    申请号:US17054263

    申请日:2019-05-09

    发明人: Lennert HEILMANN

    摘要: The invention relates to a method for applying a material (30) to a fiber composite component within an application region (13) of the fiber composite component, the fiber composite component being produced from a fiber composite material having a fiber material (11) and a matrix material (12), the method comprising the following steps: —providing at least one monofilament woven fabric (20), in which a plurality of or all threads each consist of a single filament, —arranging the at least one monofilament woven fabric (20) on a fiber preform (10) in the application region (13), which fiber preform is formed from the fiber material (11) of the fiber composite material, —curing, in a common process step, the matrix material (12) of the fiber composite material, which matrix material embeds the fibers material (11) of the fiber preform (10), and a matrix material (12) embedding the monofilament woven fabric (20), thereafter the matrix material (12) of the fiber preform (10) and the matrix material (12) of the monofilament woven fabric (20) being at least partially cured, —tearing off the monofilament woven fabric (20) integrally bonded to the fiber preform (10), and —applying the material (30) in the application region (13) after the monofilament woven fabric (20) has been torn off.

    3-D Input Device
    28.
    发明申请

    公开(公告)号:US20210103344A1

    公开(公告)日:2021-04-08

    申请号:US17044875

    申请日:2019-04-05

    IPC分类号: G06F3/0338

    摘要: A 3D input device, in particular a mobile 3D input device, has a housing and an input element arranged within the housing. The input element has at least a first side and a second side opposite the first side. The 3D input device has a sensor device. The input element is movable relative to the housing in six components. The sensor device detects the movements and/or the positions of the input element relative to the housing. The first side of the input element or the second side of the input element or the first side and the second side of the input element are together configured in such a way that a user can complete a movement of the input element along the six components via an action on the input element. A mobile device and a 3D remote-control each have at least one such 3D input device.

    Method for calibrating an active sensor system

    公开(公告)号:US10908258B2

    公开(公告)日:2021-02-02

    申请号:US16070459

    申请日:2017-01-31

    摘要: Method and system of calibrating a sensor system which comprises sensor A and sensor B. Sensor A has a transmitter TXA for emitting a signal STXA and a receiver RXA for receiving a signal SRXA, wherein RXA and TXA operate independently in a radar mode of sensor A. Sensor B has a transmitter TXB, a receiver RXB, and a unit D, which is used to connect TXB to RXB in a transponder mode of sensor B, with the result that a signal SRXB received by RXB is emitted again by TXB as a signal STXB. A gain Gcon,B between signal SRXB and signal STXB is predefined. In a radar mode of sensor B, TXB is not connected to RXB, with the result that TXB and RXB operate independently. Emitted signals may be radar, light, or acoustic signals. The method and system can calibrate radar systems, lidar systems, or sonar systems.

    METHOD AND DEVICE FOR DETERMINING THE LEADING EDGES OF TWO OVERLAPPING IMAGE CAPTURES OF A SURFACE

    公开(公告)号:US20190323838A1

    公开(公告)日:2019-10-24

    申请号:US16469097

    申请日:2017-12-07

    发明人: Daniel HEIN

    摘要: The invention relates to a method and a device (1) for determining the leading edges (S1, S2) of two overlapping image captures of a surface (OF), comprising at least one camera (2) having a matrix-type sensor (6), having n lines (7), a position and location measuring system (3), an evaluation unit (4) and a storage means (5), wherein an elevation model (H) of the surface (OF) and a projection model (P) of the camera (2) are stored in the storage means (5), which the evaluation unit (4) can access, wherein the camera position (P1, P2) in the first and second image capture is determined by means of the position and location measuring system (3), wherein a horizontal mid-point (M) between the two camera positions (P1, P2) is determined and a projection of the mid-point (M) onto the surface (OF) is carried out, wherein a back projection onto the sensor (6) is carried out in the first and second camera position (P1, P2) by means of the projection model (P) for the point (MO) determined in the above-mentioned manner and a respective pixel is determined, wherein the respective line of the sensor (6) is determined, four solid angles (RW1-4) of the respective first and last pixel (Pix1-4) of the lines (7.Z1 M0, 7.Z2M0) are determined and their leading points (SP1-SP4) are determined with the elevation model (H), mid-points (M1, M2) are determined between the leading points and projected back into the sensors in the first and second position, associated lines are determined, wherein the smallest determined line (7.MIN1) is selected as the leading edge (S1) for the first camera position (P1) and the largest determined line (7.MAX2) is selected as the leading edge (S2) for the second camera position (P2).